Ara
Toplam kayıt 22, listelenen: 11-20
Bir Gaz Türbin Motoru Kompresör PalesininTi6Al4V Alaşımından Eklemeli Üretim Yöntemi ile İmalatı ve Boyutsal Doğrulaması
(TMMOB Makina Mühendisleri Odası, 2021)
Bu çalışmada, bir gaz türbin motoruna ait kompresör palesinin, Ti6Al4V alaşımından Eklemeli Üretim
(EÜ) yöntemiyle üretimi ve boyutsal doğrulama ölçümleri gerçekleştirilmiştir. Havacılık endüstrisinde
yaygın kullanılan ...
Usage of Additive Manufacturing and Topology Optimization Process for Weight Reduction Studies in the Aviation Industry
(ASTES Publishers, 2021)
The Additive Manufacturing (AM) technology is a disruptive and novel technique that
changes the paradigm of manufacturing methodology. It is based on the principle of having
3D parts by adding simple 2D layers on and on. ...
Havacılıkta Organizasyonel Kazalar: B-737 Max Uçak Kazalarının Mühendislik Perspektifinden İncelenmesi
(TMMOB Makina Mühendisleri Odası, 2020)
Havacılık kazalarının oluşumu çoğunlukla birden fazla nedenden kaynaklanmaktadır. Diğer bir ifade ile havacılık kazaları birçok etkinin birleşiminin bir sonucu olarak meydana gelmektedir. Bu etkilere, üretim süreçleri, ...
Bir İnsansız Hava Aracının İtki ve Manevra Hareketlerinde Gövde İçi Basınçlı Hava Kullanımı
(EJOSAT, 2021)
Bu çalışmada bir İnsansız Hava Aracı (UAV) üzerinde itki sistemi olarak basınçlandırılmış havanın kullanımı sayısal determinasyon
yöntemi ile ortaya konmaktadır. Söz konusu İHA, Eklemeli Üretim (EÜ) yöntemi ile üretilecektir. ...
The Adverse Effects of Implementation of the Novel Systems in the Aviation Industry in Pursuit of Maneuvering Characteristics Augmentation System (MCAS)
(Innovare Academics Sciences Pvt. Ltd, 2020)
In the aviation history, there are many remarkable accidents. But rare of them are close to each
other with the same types of aircraft. Basically, incidents are categorized as the Controlled Flight into the
Terrain (CFIT) ...
The Temperature and Material Distribution Inside a Gas Turbine Engine
(Crimson Publishers, 2022)
The propulsion for the air vehicles is generated by the power obtained from the engines.
Especially during take-off and climb phases, the air vehicles need the maximum power.
Mainly, as presented in Figure 1, it is ...
An Experimental Determinatıon And Numerical Analysis Of A Loiter Munition Unmanned Aerial Vehicle System
(Kerim ÇETİNKAYA, 2022)
This paper experimentally determinates the calculation of an Unmanned Aerial Vehicle (UAV) and
analyzes the design criteria within four different scenarios. The UAV to be designed is a loiter munition
UAV system. A mobile ...
A Computational Determination of a Nozzle Activated Fixed-Wing Uav
(2022)
This paper proposes new methods and strategies for the propulsion of a mini Unmanned Aerial Vehicle
(UAV). Typically, the UAVs are propelled by new technology batteries, fossil fuels, and hybrid systems.
An experimental ...
Failure analysis of J85-CAN-15 turbojet engine compressor disc
(PERGAMON-ELSEVIER SCIENCE LTD, THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, ENGLAND, 2021)
This paper analyzes the J85-CAN-15 engine damage due to fracture of the compressor disc 8th
stage dovetail post. An Inner Object Damage (IOD) phenomenon was identified. The damaged
compressor disc material is Incoloy 901 ...
Fracture and Failure Analysis of the Trainer Aircraft Rudder Pedal Hanger
(ELSEVIER SCI LTD, THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, OXON, ENGLAND, 2021)
This study analyzes the T-38A Talon twin-jet trainer aircraft rudder pedal hanger damage due to
the fracture that has been identified at the clevis surfaces where the tension rises. The hanger has
the function of swinging ...